HIGH INTEGRITY ROTARY ACTUATOR AND METHOD OF OPERATION
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United States of America Patent
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Issued Date -
Sep 26, 2013
app pub date -
Mar 20, 2012
filing date -
Mar 31, 2011
priority date (Note) -
Abandoned
status (Latency Note)
Importance
Abstract
An actuator for an aircraft is provided. The actuator comprises a first motor, a second motor and an actuator output, which are interconnected by a gear assembly. The actuator output is driveable by the first motor independently of the second motor; the actuator output is driveable by the second motor independently of the first motor; and the actuator output is driveable by the first and second motors in combination.
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